|  |  |  |
| --- | --- | --- |
|   | (5) | Any and all structural repairs on the Aircraft will be permanent in nature and fully in accordance with the Manufacturer’s guidelines and will be approved where necessary by
FAA documentation. Where possible, new repairs to the fuselage skin panels will be executed by means of “flush or insert” repair methods.  |

  




|  |  |  |
| --- | --- | --- |
|   | (C) | Wings and Empennage  |

  




|  |  |  |
| --- | --- | --- |
|   | (1) | The leading edges will be free from damage, normal wear and tear excepted.  |

  




|  |  |  |
| --- | --- | --- |
|   | (2) | The wings will be free of fuel leaks.  |

  




|  |  |  |
| --- | --- | --- |
|   | (D) | Interior  |

  




|  |  |  |
| --- | --- | --- |
|   | (1) | The ceiling, sidewalls and bulkhead panels will be clean and free of cracks and stains.  |

  




|  |  |  |
| --- | --- | --- |
|   | (2) | All seat covers will be in good condition, clean and free of stains and meet applicable FAR fire regulations (burn certifications), normal wear and tear excepted.
 |

  




|  |  |  |
| --- | --- | --- |
|   | (3) | All seats will be serviceable, in good condition and recovered as necessary, normal wear and tear excepted.  |